# Service difficulty reports: N26226

A list on [N26226](https://openairdocs.org/aircraft/N26226.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 105 reports

- [SDR CALA2026091719497](https://openairdocs.org/sdr/CALA2026091719497.md): Light · inoperative · Sep 16, 2026 · N26226 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR INOP, SLAVED IN PROPERLY FUNCTIONING EMERGENCY EXIT SIGN ASSY IAW AMM 33-51-01-960-802, OPS CHECK GOOD. REQUIRES EXIT SIGN ASSY. INSTALLED NEW LIGHT ASSEMBLY, IAW AMM 33-51-01-960-802. UNIT OPS CHECKS GOOD, OK FOR SERV
- [SDR CALA2026073118131](https://openairdocs.org/sdr/CALA2026073118131.md): Bag · leaking · Jul 30, 2026 · N26226 · Boeing 737824 · Standard Practices/Structures
  > WHEN FORWARD CARGO BIN WAS OPENED THE GROUND CREW REPORTED AN ODOR OF AN UNKNOWN SUBSTANCE FIRE DEPARTMENT HAXMAT TEAM NOTIFIED. ODOR IDENTIFIED AS ACETONE. FOUND PASSENGER BAG WITH SPILLED SUBSTANCE INSIDE. REMOVED BAGS FROM FWD CARGO HOLD. ALLOWED HOLD TO
- [SDR CALA2026071617844](https://openairdocs.org/sdr/CALA2026071617844.md): Light · loose · Jul 14, 2026 · N26226 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT PATH GUIDANCE LIGHT ON 10C LOOSE AND DANGLING OUT OF THE SEAT. EMERGENCY FLOOR PROX LIGHT PLASTIC HOUSING WAS BROKEN. INSTALLED NEW PLASTIC HOUSING REF AMM 33-51-11.
- [SDR CALA2026030614377](https://openairdocs.org/sdr/CALA2026030614377.md): Proximity Sensor · faulted · Feb 28, 2026 · N26226 · Boeing 737824 · Door Warning System
  > RTO AT 70KTS FWD ENTRY DOOR LIGHT ILLUMINATED AFTER CREW DEBRIEF, CREW REPORTS NO DOOR HANDLE MOVEMENT, AIR DRAFTS OR OTHER DISCREPENCIES. INSPECTED FWD DOOR. NO ISSUES TO BE DETERMINED. OPS CHECK OF FWD ENTRY DOOR NORMAL. INDICATION ISSUE SUSPECTED. AMM 52-11
- [SDR CALA2026021313766](https://openairdocs.org/sdr/CALA2026021313766.md): Battery Pack · no test · Feb 11, 2026 · N26226 · Boeing 737824 · Emergency Lighting
  > OPS CHECK OF EMERGENCY LIGHTS, DURING CHECK, FOUND RT AFT EMERGENCY OVERWING LIGHT OUT. EXTERIOR OVERWING LIGHT INOPERATIVE. REPLACED THE LAMP IN RT AFT OVERWING EMERGENCY LIGHT TWO TIMES. NO HELP. IAW AMM 33-51-04-960-801, R & R THE M1695 CHARGER & BATTERY
- [SDR CALA2025122912503](https://openairdocs.org/sdr/CALA2025122912503.md): Slide · out of adjust · Dec 25, 2025 · N26226 · Boeing 737824 · Escape Slide
  > ESCAPE SLIDE PACK BUSTLE DAMAGED. L2 SLIDE FABRIC EXPOSED. INSPECTED AND ADJUSTED MATERIAL IAW AMM 25-66-01-400-803. NO DEFECTS NOTED.
- [SDR CALA2025110210824](https://openairdocs.org/sdr/CALA2025110210824.md): Battery Pack · discharged · Nov 1, 2025 · N26226 · Boeing 737824 · Emergency Lighting
  > SUPPORT TASK EMERGENCY BATTERY M1676 HAS LOW VOLTAGE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1676 IAW AMM 33-51-06-960-805. EMERGENCY LIGHT BATTERY PACK M1676 OPS CHECKS GOOD IAW AMM 33-51-06-960-805.
- [SDR CALA2025110210799](https://openairdocs.org/sdr/CALA2025110210799.md): Oxygen Mask · no test · Oct 29, 2025 · N26226 · Boeing 737824 · Passenger Oxygen System
  > RIGHT AFT GALLEY MANUAL OXYGEN DEPLOYMENT DROP FAILED. RT AFT GALLEY OXYGEN BOX DOOR AND OXYGEN PASSENGER RIGHT CIRCUIT BREAKER IAW AMM 35-22-00-700-802. RT AFT GALLEY MANUAL OXYGEN OPS TESTED GOOD IAW AMM 35-22-00-700-802.
- [SDR CALA2025110210797](https://openairdocs.org/sdr/CALA2025110210797.md): Oxygen Mask · no test · Oct 29, 2025 · N26226 · Boeing 737824 · Passenger Oxygen System
  > LEFT SEAT 34 MANUAL OXYGEN DEPLOYMENT DROP FAILED. SEAT 34ABC OXYGEN BOX DOOR ON PSU AND OXY INDICATOR AND OXYGEN PASSENGER LEFT CIRCUIT BREAKERS IAW AMM 35-22-00 -700-802. MANUAL OXYGEN DEPLOY OPS TEST GOOD IAW AMM 35-22-00-700-802.
- [SDR CALA2025110210795](https://openairdocs.org/sdr/CALA2025110210795.md): Oxygen Mask · no test · Oct 29, 2025 · N26226 · Boeing 737824 · Passenger Oxygen System
  > RIGHT SEAT 1 MANUAL OXYGEN DEPLOYMENT DROP FAILED. RECYCLED SEAT 1EF O2 BOX DOOR ON PSU AND O2 IND AND O2 PASSENGER RH CB IAW AMM 35-22-00-700-802. MANUAL O2 MASK OPS CHECK GOOD IAW B737-800 AMM 35-22-00-700-802.
- [SDR CALA2025110610946](https://openairdocs.org/sdr/CALA2025110610946.md): Skin · damaged · Oct 28, 2025 · N26226 · Boeing 737824 · Cargo/Baggage Doors
  > FWD CARGO DOOR SKIN REPLACED DUE TO DAMAGE. REMOVED AND REPLACED OUTER SKIN IAW DWG 143A69110, REV D, SRM 52-30-01-2R-3, REPAIR 3, AND CMM 52-31-15.
- [SDR CALA2025102910700](https://openairdocs.org/sdr/CALA2025102910700.md): Deck Plate · dented · Oct 23, 2025 · N26226 · Boeing 737824 · Fuselage Main, Structure
  > FLIGHT DECK FLOOR HAS DENTS BETWEEN BS 250 & 260, BEWTEEN LBL-18 & RBL 10. DENT WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1. W=4.2 DEPTH OF DAMAGE 0.016 ORIG THICK 0.040 REMAIN 0.024. FABRICATED (1 EA -1 WEB) AND (2 EA -2 SPLICE DOUBLER) IAW REO G25
- [SDR CALA2025110610936](https://openairdocs.org/sdr/CALA2025110610936.md): Skin · damaged · Oct 22, 2025 · N26226 · Boeing 737824 · Cargo/Baggage Doors
  > AFT CARGO DOOR SKIN DAMAGED. REMOVED AND REPLACED AFT CARGO DOOR OUTER SKIN IAW DWG 146A6110 REV C AND SRM 52-30-01-2R-3.
- [SDR CALA2025102710556](https://openairdocs.org/sdr/CALA2025102710556.md): Window Frame · cracked · Oct 18, 2025 · N26226 · Boeing 737824 · Fuselage Main, Structure
  > LEFT NR 3 WINDOW POST HOLE NR 3 IS CRACKED IN THE 3 AND 9 O'CLOCK POSITION. ACCOMPLISHED REO-G25600 ACCOMPLISHED REPAIR AT FLIGHT DECK LT NR 3 WINDOW POST,REMOVED DAMAGED,FABBED AND INSTALLED -1 DOUBLER -2 TRIPLER,-3 FILLER, AND INTERNAL DOUBLER IAW REO:G256
- [SDR CALA2025102110332](https://openairdocs.org/sdr/CALA2025102110332.md): Housing · gouged · Oct 17, 2025 · N26226 · Boeing 737824 · Passenger/Crew Doors
  > L-2 DOOR HANDLE BOX CUTOUT UPPER BUSHING AREA IS GOUGED. REMOVED AND REPLACED STUB BEAM IAW BAC DWG 147A6116 REV -.
- [SDR CALA2025110710992](https://openairdocs.org/sdr/CALA2025110710992.md): Frame · punctured · Oct 14, 2025 · N26226 · Boeing 737824 · Fuselage Main, Frame
  > MAIN CABIN STA 259.5 FRAME IS PUNCTURED IN LINE WITH S12L. REPAIRED AREA IAW REO G25625 AND IN CONJUNCTION WITH ECRA 5312-01199 AND SRM 51-40-02. PER ECRA 5312-01199 THIS IS A MAJOR REPAIR. CREATED ESFR REFERENCE DIP LP 6620459 APPROVED. REFER TO DIP 6620459 A
- [SDR CALA2025102610540](https://openairdocs.org/sdr/CALA2025102610540.md): Frame · gouged · Oct 14, 2025 · N26226 · Boeing 737824 · Fuselage Main, Frame
  > MAIN CABIN LH SIDE STA. 380 FRAME, APPROX. 12" FROM THE FLOOR IS GOUGED. PER ECRA 5332-01029 BLENDED AREA TO REMOVE GOUGE.GOUGE REMOVED BUT FOUND TO BE OUT OF LIMITS IAW SRM 53-30-07-01. FABRICATED REPAIR IAW SRM 53-00-07. APPLIED ALODINE AND PRIMER IAW B737
- [SDR CALA2025101309954](https://openairdocs.org/sdr/CALA2025101309954.md): Floorbeam · corroded · Oct 9, 2025 · N26226 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM UPPER TEE ANGLE HAS CORROSION AT BS 380 RBL 0. REMOVED CORROSION IAW IAW SRM 53-30-51. FOUND TO BE OUT OF LIMITS IAW 53-36-51, ORIG.125, MAT LOSS.038, REM.087 FABRICATED A STRAP AND FILLERS IAW REO-G25602 AND REO-25602 FIGURE 2. ALOD
- [SDR CALA2025101309953](https://openairdocs.org/sdr/CALA2025101309953.md): Floorbeam · corroded · Oct 9, 2025 · N26226 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN FWD WET AREA FLOORBEAM, STA 312 LBL45 HAS CORROSION. CUT OUT CORRODED SECTION OF TEE CHORD AND REPAIRED WITH TEE CHORD, ANGLES AND STRAPS IAW SRM 53-10-51. REPAIR 12
- [SDR CALA2025101309946](https://openairdocs.org/sdr/CALA2025101309946.md): Seat Track · corroded · Oct 8, 2025 · N26226 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN AFT WET AREA STA 891, LBL 46, SEAT TRACK FITTING AT FASTENER HAS CORROSION. REMOVED CORROSION FROM SEAT TRACK.020 REMOVED, 05 REMAINING AREA OUT OF LIMITS & SRM 53-00-52. REMOVED OLD SEAT TRACK PER AIPC 53-42-11-34. INSTALLED NEW SEAT TRACK PER AI
- [SDR CALA2025101309945](https://openairdocs.org/sdr/CALA2025101309945.md): Web · corroded · Oct 7, 2025 · N26226 · Boeing 737824 · Fuselage Miscellaneous Structure
  > LEFT AFT WET AREA BS 987 FLOOR WEB HAS AREAS OF CORROSION.. REMOVE AND REPLACED FLOOR WEB AND REMOVED AND REINSTALLED 1EA ZEE ANGLE AND 2EA GALLEY FITTINGS TO FOM IAW SRM 51-40-02, BAC DWG NO. 147A5700 REV:B AND AMM 20-50-11-910-801 TABLE 204 AND 205, & DWG
- [SDR CALA2025100909844](https://openairdocs.org/sdr/CALA2025100909844.md): Stub Beam · worn · Oct 7, 2025 · N26226 · Boeing 737824 · Passenger/Crew Doors
  > L1 DOOR HANDLE BOX CUTOUT, UPPER TORQUE TUBE BUSHING AREA, STUB BEAM IS GOUGED. REMOVED GOUGED STUB BEAM IAW B737-800 SRM 51-40-02. LOCATED, DRILLED AND INSTALLED NEW STUB BEAM PN 141A6143-6 IAW BAC DWG 141A6190 REV E AND B737-800 SRM 51-40-02 AND BAC DWG 141
- [SDR CALA2025100909842](https://openairdocs.org/sdr/CALA2025100909842.md): Stop Fitting · worn · Oct 7, 2025 · N26226 · Boeing 737824 · Passenger/Crew Doors
  > L-2 DOOR UPPER FWD DOOR STOP FITTING IS GOUGED. REPAIR COMPLETED STATUS CHANGE FROM MAJOR REMOVED AND REPLACED L-2 DOOR UPPER FWD DOOR STOP FITTING IAW BAC DWG 147A6125 AND BAC DWG 147A6116 REV -.
- [SDR CALA2025100709737](https://openairdocs.org/sdr/CALA2025100709737.md): Intercostal · corroded · Oct 4, 2025 · N26226 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA STA 952, RBL26, INTERCOSTAL ANGLE HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL PER BAC DWG 147A5660 ID:0014 REV:- T05867-173.
- [SDR CALA2025102910692](https://openairdocs.org/sdr/CALA2025102910692.md): Skin · worn · Oct 2, 2025 · N26226 · Boeing 737824 · Fuselage Main, Plate/Skin
  > FUSELAGE INTERIOR SKIN CHAFED, FORWARD OF L1 DOOR IN TORQUE TUBE AREA. REMOVED AND REPLACED L1 DOOR MIDDLE HINGE GAP COVER IAW DWG 141A3112 REV A, DWG 141A3110 REV-, AND SRM 51-40-02 RESTORED PROTECTIVE FINISH IAW AMM 51-21-73.
- [SDR CALA2025102910690](https://openairdocs.org/sdr/CALA2025102910690.md): Stringer Splice · corroded · Oct 2, 2025 · N26226 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > E&E COMPT, STRINGER SPLICE CORRODED BETWEEN STA 360 AND 380, 17.5" LBL. REPAIRED THE STRINGER SPLICE AND NEW STRINGER SECTIONS IN THE E&E COMP AT STA 360 STRINGER 27L IAW SRM 53-00-03-2R-1.
- [SDR CALA2025102910688](https://openairdocs.org/sdr/CALA2025102910688.md): Floor Support · corroded · Oct 2, 2025 · N26226 · Boeing 737824 · Fuselage Miscellaneous Structure
  > RIGHT AFT WET AREA BS 947-967 FLOOR SUPPORT HAS AREAS OF CORROSION. REMOVED, LOCATED, DRILLED, & REPLACED THE FLOOR SUPPORT IAW DWG 147A5760, REV-.
- [SDR CALA2025102910686](https://openairdocs.org/sdr/CALA2025102910686.md): Floorbeam · corroded · Oct 2, 2025 · N26226 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM BS 986, RBL 34-44 HAD CORROSION ON UPPER SURFACE. REMOVED AND REPLACED EXISTING CORRODED TEE ANGLE REPAIR AT BS 987 FROM RBL 50 TO LBL 30 IAW SRM 53-70-51-2R-4, REPAIR 4.
- [SDR CALA2025102910684](https://openairdocs.org/sdr/CALA2025102910684.md): Floorbeam · corroded · Oct 2, 2025 · N26226 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT WET AREA FLOORBEAM STA 947.5 RBL50 HAS CORROSION. REMOVED AND EVALUATED DAMAGE 50 PERCENT MAT LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1.CUTTOUT DAMAGED AREA AND REPAIRED WITH TEE CAP ANGLES, AND STRAPS PER SRM 53-70-51-2R-5.
- [SDR CALA2025102610520](https://openairdocs.org/sdr/CALA2025102610520.md): Skin · cracked · Oct 2, 2025 · N26226 · Boeing 737824 · Galley Doors
  > R-1 DOOR,WINDOW CAVITY,INNER SKIN, LOWER FORWARD CORNER IS CRACKED. COMPLETED ESFR REMOVED AND REPLACED R-1 DOOR UPPER INNER SKIN IAW BAC DWG 141A6516 REV F.
- [SDR CALA2025100609642](https://openairdocs.org/sdr/CALA2025100609642.md): Web · corroded · Oct 2, 2025 · N26226 · Boeing 737824 · Fuselage Miscellaneous Structure
  > RIGHT AFT WET AREA FROM BS 987 - 992 FLOOR WEB HAS AREAS OF CORRISION. REMOVED AND REPLACED CORRODED AFT CORNER WEB AT STA 987 RBL 45 IAW BAC DWG NO.147A5700 REV:B AND B737-800 SRM 51-40-02.
- [SDR CALA2025100109492](https://openairdocs.org/sdr/CALA2025100109492.md): Floor Support · corroded · Sep 29, 2025 · N26226 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN, BS 312-328 LBL12, FLOOR SUPPORT CORRODED ON UPPER SURFACE. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-51 7A-1 ORIG..086 REMOVED.015 REMAINING.065.. INSTALLED AN NEW FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A
- [SDR CALA2025092609297](https://openairdocs.org/sdr/CALA2025092609297.md): Crease Beam · corroded · Sep 24, 2025 · N26226 · Boeing 737824 · Fuselage Main, Structure
  > MAIN CABIN AFT WET AREA CREASE BEAM LBL 60 HAS CORROSION BETWEEN BS 947 & 993. ORIGINAL DAMAGE ON INNER CHORD FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1. REMOVED AND REPLACED INNER CHORD IAW SRM 51-40-02, DWG 147A8540, REV B, & DWG 147A8501, REV C.
- [SDR CALA2025102910682](https://openairdocs.org/sdr/CALA2025102910682.md): Floor Support · corroded · Sep 17, 2025 · N26226 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA BS 947-967, LBL 24, INTERCOSTAL HAS CORROSION, REPAIR IS CLASSIFIED AS MAJOR, REPLACED IAW SRM 51-40-02 AND DRAWING 147A5650, REV C. REMOVED DAMAGE IAW SRM 53-70-51. ORIGINAL THICKNESS.080 MAT LOSS 0.060. FOUND TO BE OUT OF LIMITS IA
- [SDR CALA2025072206844](https://openairdocs.org/sdr/CALA2025072206844.md): Hmu · faulted · Jul 20, 2025 · N26226 · Boeing 737824 · Fuel Controlling System
  > MENTIONED TO MX TECH NUM TWO ENG LAGGED AFTER TOGA. ALMOST 30-40 SPLIT AT ONE POINT UPDATE LABOR HOURS REPLACED HYDROMECHANICAL UNIT PER AMM 73-21-10/401. ACCOMPLISHED POWER PLANT RUN TEST REFERENCE TABLE ( TASK 71-00-00-800-811-F00.
- [SDR CALA2025041403788](https://openairdocs.org/sdr/CALA2025041403788.md): Bulkhead · cracked · Apr 11, 2025 · N26226 · Boeing 737824 · Fuselage Main, Bulkhead
  > DURING WALK AROUND FOUND CRACK IN UPPER WHEEL WELL FORWARD BULKHEAD JUST AFT OF RESERVOIR B GAUGEWALK AROUND PERFORMED FOR ETOPS CK VERIFIED AND MARKED CRACK ENDS USING NDT 6-51-00-00-23. DURING ETOPS WALK AROUND FOUND CRACK IN UPPER RIGHT WHEEL WELL, FORWARD
- [SDR CALA2025032003040](https://openairdocs.org/sdr/CALA2025032003040.md): Extinguisher · leaking · Mar 17, 2025 · N26226 · Boeing 737824 · Fire Bottle, Portable
  > COCKPIT HALON FIRE EXTINGUSHER HAD SLOW LEAK WHILE AIRBORNE. SWAPPED THE AFT CABIN OVER SEAT 37 HALON FIRE EXTINGUISHER WITH THE DEPLETED ON IN THE FLIGHT DECK PLACING THE FWD GALLEY HALON FIRE EXTINGUISHER ON MEL 2603A. RETURNED PREVIOUSLY SWAPPED FIRE
- [SDR CALA2025031102709](https://openairdocs.org/sdr/CALA2025031102709.md): Anti-Ice Valve · faulted · Mar 8, 2025 · N26226 · Boeing 737824 · Engine Anti-Icing System
  > NUMBER 2 ENGINE COWL ANTI ICE LIGHT ILLUMINAT INFLIGHT. RAN THE CHECK LIST AND IT WOULD NOT REMOVED & REPLACED #2 ENG ANTI ICE COWL VALVE REF AMM 30-21-11, NO HELP. SUSPECT #2 ENG OVERPRESSURE SWITCH REQUIRES REPLACEMENT, DEFER TO MEL 3003D. #2 ENG COWL ANT
- [SDR CALA2025030302553](https://openairdocs.org/sdr/CALA2025030302553.md): Door · out of adjust · Mar 1, 2025 · N26226 · Boeing 737824 · Passenger/Crew Doors
  > DURING DOOR SLIDE REPLACEMENT, FOUND DOOR 2L WITH EXCESSIVE LATERAL PLAY. FOUND GIRT BAR HITTING JUMPSEAT AND DOOR HITTING FRAME ON UPPER LH SIDE. ACPED ADJUSTMENT OF AFT ENTRY DOOR GUIDE ARM; FWD LOWER LATCH RECEIVER; HORIZONTAL CONTROL ROD; UPPER GATE CONTRO
- [SDR CALA2025030302552](https://openairdocs.org/sdr/CALA2025030302552.md): Block · damaged · Mar 1, 2025 · N26226 · Boeing 737824 · Escape Slide
  > ESCAPE SLIDE INSTALL {B737-25-3-3636} - SLIDE LATCH BLOCK DAMAGED. REF AMM TASK 25-66-01-400-801. REPLACED LATCH BLOCK. RELEASE REQUIREMENTS PASSED. REF AMM 25-66-01-400-801 AND TASK CARD 29-0525-8-0697.PARTS USED: 99-2560-3-0163, QTY:1
- [SDR CALA2025010101735](https://openairdocs.org/sdr/CALA2025010101735.md): Unknown · odor · Jan 2, 2025 · N26226 · Boeing 737824 · Air Distribution System
  > FA REPORTS SMOKE ODOR IN CABIN. DEBRIEFED FLIGHT CREW AND CABIN CREW. SOURCE OF ODOR IS UNIDENTIFIED. CABIN CREW WAS UNABLE TO PROVIDE AN ACCURATE DESCRIPTION OF WHAT IT SMELLED LIKE. FLIGHT CREW STATES THAT CABIN CREW REPORTED ODOR WHEN ENGINE POWER SETTINGS
- [SDR CALA2025010200012](https://openairdocs.org/sdr/CALA2025010200012.md): Unknown · odor · Jan 1, 2025 · N26226 · Boeing 737824 · Air Distribution System
  > FA REPORTS SMOKE ODOR IN CABIN. AND CABIN TEMP CONTROL WAS ADJUSTED. CABIN CREW STATES THAT ODOR ENGINES AS THE BLEED SOURCE. OPERATED TEMP CONTROL THRU THE DECREASED WHEN CABIN TEMP CONTROL WAS CHANGED TO FULL COLD. DIFFERENT CONFIGS PER THE FIM TASK WITH NO
- [SDR CALA2024042401216](https://openairdocs.org/sdr/CALA2024042401216.md): Anti-Ice Valve · failed · Apr 21, 2024 · N26226 · Boeing 737824 · Engine Anti-Icing System
  > RIGHT ENGINE ANTI ICE VALVE FAILED TO OPEN IN FLIGHT NOT ENOUGH GROUND TIME FOR FURTHER T/S. REQUESTING MEL. POSITIONED SHUTOFF VALVE IN THE OPEN POSITION AND DISCONNECED, OVERPRESSURE SWITCH. PLACARD INSTALLED. PLACING ON MEL. CAPPED AND STOWED THE ELECTRICAL
- [SDR CALA2024031800753](https://openairdocs.org/sdr/CALA2024031800753.md): Fairing · missing · Mar 15, 2024 · N26226 · Boeing 737824 · Aerodynamic Fairings
  > PDA 1 REF LP 7357370 LEFT WING TO BODY FAIRING PANEL 193CL FOUND MOSTLY MISSING AND PARTIALLY DAMAGED ON WALK AROUND. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CONT
- [SDR CALA2023012300191](https://openairdocs.org/sdr/CALA2023012300191.md): Shutoff Valve · faulted · Jan 23, 2023 · N26226 · Boeing 737824 · Pneumatic Distribution System
  > DUCT PRESSURE INDICATION L AND R POINTERS NOT THE SAME (SPLIT), WITH EITHER POINTER BELOW 18 PSIG DURING TAKEOFF, CLIMB AND CRUI SE; THE ENGINE IS THE BLEED SOURCE LEFT PACK 45 RIGHT PACK 6-8 PSI IN CLIMB OUT REF FIM 36-10 TASK 804 PERFORMED PNEUMATIC HEALTH C
- [SDR CALA2023010400019](https://openairdocs.org/sdr/CALA2023010400019.md): None · none · Jan 4, 2023 · N26226 · Boeing 7378 · Standard Practices/Structures
  > ROBBED AFT LEFT EMERGENCY LIGHT POWER SUPPLY BATTERY REF AMM 33-51-06-960-806. C/B''S PULLED AND TAGGED. ROBBED PARTS TAG SECURED ON CANNON PLUG AT AFT GALLY AREA. REPLACED BATTERY PACK FOR POWER SUPPLY IN AFT GALLEY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.PA
- [SDR CALA2022121903429](https://openairdocs.org/sdr/CALA2022121903429.md): Stringer · none · Dec 18, 2022 · N26226 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > LOG PAGE CREATED FOR SFR REPORTING ONLY, STRINGER 25L IS CORRDED BETWEEN FRAMES STATIONS 827 AND 847. REF BAM LOG PAGE 001136824 FOR DISCREPANCY AND CORRECTIVE ACTION ESFR CREATED AND APPROVED, NR FOR REPORTING ONLY.
- [SDR CALA2021102001924](https://openairdocs.org/sdr/CALA2021102001924.md): None · none · Oct 18, 2021 · N26226 · Boeing 737824 · Fuselage Structure (General)
  > DOOR 1L BELOW FLOOR LINE AT STATION 351 DENT 3 1/2 INCH BY 1 INCH. REMOVED RIVETS AT STA375 STR-18L REF: AVO9227 REPAIRS ACPD PER AVO 09227B AND ECRA 5310-07925. MAJOR REPAIR REPORT ON LP 7265510.
- [SDR CALA2021070901048](https://openairdocs.org/sdr/CALA2021070901048.md): Fitting · cracked · Jul 7, 2021 · N26226 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STA 540AND LBL 40.87 IS CRACKED. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 AND LBL 40.87 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX NR 00085 AND HANGER NR 5866643 DATA WAS TRANSCRIBED F
- [SDR CALA2021070901047](https://openairdocs.org/sdr/CALA2021070901047.md): Fitting · cracked · Jul 7, 2021 · N26226 · Boeing 737824 · Wing Structure
  > B737-57-4-1262 SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND RBL 15.04 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R 00090 AND HANGER N/R 5865978 FOR WORK ACCOMPLISHED. DATA WAS T

Next page: https://openairdocs.org/aircraft/N26226/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N26226' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N26226/reports

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